EP3312082B1 - Aéronef à portes multiples - Google Patents
Aéronef à portes multiples Download PDFInfo
- Publication number
- EP3312082B1 EP3312082B1 EP16400046.5A EP16400046A EP3312082B1 EP 3312082 B1 EP3312082 B1 EP 3312082B1 EP 16400046 A EP16400046 A EP 16400046A EP 3312082 B1 EP3312082 B1 EP 3312082B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aircraft
- door
- real
- image formation
- vehicle door
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000015572 biosynthetic process Effects 0.000 claims description 52
- 238000012806 monitoring device Methods 0.000 claims description 16
- 238000011179 visual inspection Methods 0.000 description 16
- 238000007689 inspection Methods 0.000 description 4
- 238000009413 insulation Methods 0.000 description 3
- 230000008054 signal transmission Effects 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000006748 scratching Methods 0.000 description 2
- 230000002393 scratching effect Effects 0.000 description 2
- 238000012800 visualization Methods 0.000 description 2
- 230000004913 activation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002085 irritant Substances 0.000 description 1
- 231100000021 irritant Toxicity 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B41/00—Locks with visible indication as to whether the lock is locked or unlocked
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
- B64C1/1423—Passenger doors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
Definitions
- the invention is related to a vehicle door with at least one lock lever that is provided for engaging a counterpart in an engaged state for locking the vehicle door at the associated vehicle.
- the invention is further related to an aircraft with a plurality of aircraft doors, each aircraft door comprising at least one lock lever that is provided for engaging a counterpart in an engaged state for locking a respective aircraft door relative to the aircraft.
- aircraft doors must fulfil predefined airworthiness requirements in order to allow for a safe, secure and reliable operation of respective aircrafts.
- airworthiness requirements are defined in applicable safety regulations and specifications, such as the US-American Federal Aviation Regulations (FAR) and/or the European Certification Specifications (CS) from the European Aviation Safety Agency (EASA).
- each aircraft door must be provided with means that allow for a direct visual inspection of an underlying door locking mechanism in order to determine whether the aircraft door is fully closed, latched and locked.
- a direct visual inspection is requested, as dispatch of a given aircraft may be permitted in some circumstances even if a flight deck indication, or other remote indication, of an unsafe aircraft door persists although all aircraft doors of the given aircraft are fully closed, latched and locked. In such circumstances, the dispatch should, nevertheless, not lead to hazardous or uncontrollable operation conditions of the given aircraft.
- a direct visual inspection could e. g. be performed by providing a given aircraft door with one or more suitable viewing ports. More specifically, a viewing port could be provided that allows to visualize an underlying door locking mechanism of the given aircraft door through a respective door lining and insulation. However, such a viewing port is neither considered aesthetically pleasant, nor practically feasible in all circumstances.
- indirect viewing for a visual inspection of an underlying door locking mechanism of a given aircraft door implies use of a mechanical arrangement that determines a respective mechanism status of the underlying door locking mechanism of the given aircraft door by using e. g. levers, shafts and drive pins that are interconnected to activate an indication flag that indicates the respective mechanism status, so that a reliable, positive indication of the respective mechanism status of the underlying door locking mechanism can be obtained.
- a mechanical arrangement usually implements an indication arrangement that comprises a mechanism that drives an indicator flag.
- a shaft in turn is provided with an indicator flag, which rotates behind an indicator plate.
- a slot in this indicator plate provides viewing access to a small area of the flag, which conventionally comprises a green and a red section. If the green section shows up in the slot, the underlying door locking mechanism is supposed to be in locked state and, if the red section shows up in the slot, the underlying door locking mechanism is supposed to be in unlocked state.
- security systems which allow to prevent an inadvertent deployment of aircraft doors or which allow a direct or indirect viewing of aircraft equipment from an inside of a given aircraft. Exemplary security systems are briefly discussed hereinafter.
- the document WO 2014/167038 A1 describes a security system that comprises video cameras for producing real-time images and, more particularly, videos of a surrounding of a given aircraft.
- the video cameras i. e. respective camera lenses, replace aircraft windows and, more particularly, windows in aircraft doors.
- the security system further comprises illumination sources for illuminating the surrounding in at least one radiation range, respectively.
- this security system is not suitable for determining whether a given aircraft door is fully closed, latched and locked.
- the document CA 2 769 796 A1 describes a similar security system in the form of a cockpit video system with multiple video cameras, a video processing module and a monitor.
- the video cameras are attached to an exterior of a given aircraft for producing real-time images and, more particularly, videos of a surrounding of the given aircraft.
- the video cameras would be used to show the aircraft doors, this would only be suitable to determine whether the aircraft doors are fully closed, but not for determining whether the aircraft doors are latched and locked.
- the document DE 10 2008 059 123 A1 describes a security system that is implemented by means of an inspection apparatus that comprises a mirror arrangement used for visualizing outside components of a given aircraft. However, even if the inspection apparatus would be used to show the aircraft doors, this would only be suitable to determine whether the aircraft doors are fully closed, but not for determining whether the aircraft doors are latched and locked.
- An exemplary visual inspection device in the field of down holes is e. g. described in the documents US5519543 , WO2004030336 and US6659401 .
- an object of the present invention to provide a new aircraft door and, more generally, a new vehicle door, which allows for a simplified, secure, safe and reliable determination of an associated latched and locked state. Furthermore, it is an object of the present invention to provide a new aircraft having such a new aircraft door.
- a vehicle door with at least one lock lever that is provided for engaging a counterpart in an engaged state for locking the vehicle door at the associated vehicle, said vehicle door comprising the features of claim 1.
- the object is further solved by an aircraft with a plurality of aircraft doors, each aircraft door comprising at least one lock lever that is provided for engaging a counterpart in an engaged state for locking a respective aircraft door relative to the aircraft, said aircraft comprising the features of claim 10.
- the present invention provides a vehicle door with at least one lock lever that is provided for engaging a counterpart in an engaged state for locking the vehicle door at the associated vehicle.
- a real-time monitoring device is provided for generating a real-time representation of the at least one lock lever and the counterpart, the real-time representation being suitable for determining whether the at least one lock lever is in the engaged state.
- the at least one lock lever of the vehicle door and the counterpart are key mechanism elements of a respective door locking mechanism, which are essential for door locking. Therefore, these two key mechanism elements are preferably marked and a respective alignment of their markings will show without ambiguity that the two key mechanism elements are correctly engaged in each other, and therefore locking of the vehicle door is ensured.
- an image formation device is provided and, preferably, mounted adjacent to the at least one lock lever of the vehicle door and the counterpart, preferentially on or in a respective door structure.
- the image formation device will relay a respective status of the at least one lock lever of the vehicle door and the counterpart to a display device, which is either arranged on the vehicle door, adjacent to the vehicle door within a vehicle cabin of the associated vehicle, or directly in a respective vehicle cockpit.
- Arrangement of the display device directly on the vehicle door may advantageously be used for relaying also current conditions outside of the vehicle door, if a further image formation device is provided by means of a camera system that replaces a conventional door window.
- the image formation device comprises an integrated backlight to ensure visibility under all external or internal lighting conditions.
- a respective lens of the image formation device is preferably coated to provide resistance to scratching, to prevent fogging and to ensure resistance to fluids commonly used in the operation and cleaning of vehicles, in particular aircrafts.
- the image formation device preferably utilizes an already existing power supply that is e. g. running through an existing door wire harness.
- the real-time monitoring device by provision of the real-time monitoring device a comparatively large reduction in respectively required space for its implementation compared to available prior art means results, leading to more available space inside an underlying door structure for other door systems and less intrusion beyond an inner mould line into the associated vehicle.
- the visual inspection provision by means of the real-time monitoring device may not only be available in the vicinity of the vehicle door, it could also be relayed to a screen anywhere in the associated vehicle.
- the real-time monitoring device comprises an image formation device.
- the image formation device comprises at least video formation capabilities, wherein the real-time representation is a video.
- the image formation device further comprises still image formation capabilities, wherein the real-time representation is switchable between the video and a still image.
- a fixation member is provided that rigidly attaches the image formation device to a door structure of the vehicle door.
- a control panel is provided for controlling operation of the image formation device.
- control panel comprises a display screen for displaying the real-time representation.
- the image formation device comprises a backlight device.
- the associated vehicle is an aircraft, wherein the vehicle door defines a cabin access door of the aircraft.
- the complete conventional indication arrangement as described above can be omitted in this case.
- significant cost and weight savings could be achieved.
- no moving parts are required that could be subject to wear and tear.
- the visual inspection provision would not only be available in the vicinity of the aircraft door. Instead, it could also be relayed to a screen anywhere in the aircraft, e. g. to another crew member on the flight deck.
- a respective lining provided in the region of the real-time monitoring device could significantly be simplified compared to the lining that is required for the conventional indication arrangement and, in particular, a lining and/or insulation reduction is no longer required. More specifically, a grow-out or viewing port for the indicator flag would no longer be required.
- any cut-out in the lining and an associated insulation cut-out which is a potential source for cold spots, cold air drafts and moisture into the aircraft cabin, can advantageously be omitted. In particular, such cold spots, cold air drafts and moisture into the aircraft cabin are considered irritants to passengers and cabin crew alike, so that avoidance thereof is beneficial.
- the present invention further provides an aircraft with a plurality of aircraft doors.
- Each aircraft door comprises at least one lock lever that is provided for engaging a counterpart in an engaged state for locking a respective aircraft door at the aircraft.
- a real-time monitoring device is provided for generating a real-time representation of the at least one lock lever and the counterpart, the real-time representation being suitable for determining whether the at least one lock lever is in the engaged state.
- the respective aircraft door is a cabin access door.
- the real-time monitoring device comprises an image formation device that comprises at least video formation capabilities, wherein the real-time representation is a video.
- the image formation device further comprises still image formation capabilities, wherein the real-time representation is switchable between the video and a still image.
- At least one display screen is provided for displaying the real-time representation.
- the at least one display screen is provided at the respective aircraft door, in vicinity of the respective aircraft door and/or on an aircraft flight deck of the aircraft.
- Figure 1 shows an aircraft 1 with an aircraft airframe 2.
- the aircraft 1 illustratively comprises a passenger cabin 3a, a cargo deck 3b and a flight deck or cockpit 3c.
- the aircraft 1 is accessible via a plurality of doors 4, which exemplarily comprises several cabin access doors 4a, 4b, 4c and 4d, as well as one or more cargo deck access doors 4e.
- the passenger cabin 3a and the flight deck 3c are accessible via the cabin access doors 4a, 4b, 4c and 4d
- the cargo deck 3b is accessible via the one or more cargo deck access doors 4e.
- the plurality of doors 4 is preferably adapted to close the airframe, i. e. fuselage 2 of the aircraft 1, preferentially in a fluid-tight manner.
- at least one and preferably each one of the plurality of doors 4 is embodied for allowing a determination of a respective current operation state thereof by means of a visual inspection. This visual inspection is preferentially suitable for determining whether a respective one of the plurality of doors 4 is fully closed, latched and locked.
- the aircraft 1 is an airplane.
- the present invention is not limited to airplanes.
- any vehicle that may be equipped with doors that allow a visual inspection of a respective current operation state thereof are likewise contemplated.
- the present invention may alternatively be applied to vessels, such as ships and so on. Consequently, the present invention is not limited to aircraft doors, but can likewise be applied to any arbitrary vehicle door.
- the present invention is hereinafter described with respect to aircraft doors and, only exemplarily, to aircraft cabin access doors.
- FIG 2 shows the cabin access door 4d of Figure 1 , which is hereinafter described in more detail.
- the cabin access door 4d is merely described representatively for all aircraft doors 4a, 4b, 4c, 4e of the aircraft 1 of Figure 1 .
- the cabin access door 4d is even more generally only described by way of example for an arbitrary vehicle door, to which the present invention can be applied.
- the cabin access door 4d comprises at least one lock lever 6 that is provided for engaging a counterpart 7 in an engaged state for locking the cabin access door 4d relative to the aircraft 1 of Figure 1 .
- the at least one lock lever 6 is preferably moveably mounted to an associated door structure 5 of the cabin access door 4d and the counterpart 7 is preferably also mounted to the associated door structure 5, preferentially also moveably, but may alternatively also be mounted rigidly or moveably to the aircraft airframe 2 of Figure 1 .
- the at least one lock lever 6 and the counterpart 7 are considered as being the key mechanism elements of a respective door locking mechanism, which are essential for door locking. In other words, when the at least one lock lever 6 and the counterpart 7 are correctly engaged in each other, locking of the cabin access door 4d is considered as being ensured.
- a particular implementation of the at least one lock lever 6 and the counterpart 7 are not part of the present invention, as they are well-known to the person skilled in the art.
- a detailed implementation of the respective door locking mechanism as such is also not part of the present invention and well-known to the person skilled in the art. Thus, more detailed descriptions thereof are omitted for brevity and conciseness of the description.
- the cabin access door 4d comprises a real-time monitoring device 8 that is provided for generating a real-time representation 12 of the at least one lock lever 6 and the counterpart 7.
- the real-time monitoring device 8 comprises an image formation device 8b that is preferentially rigidly attached to the associated door structure 5 of the cabin access door 4d by means of a fixation member 8a, e. g. a dedicated support bracket.
- the image formation device 8b preferably comprises at least video formation capabilities.
- the image formation device 8b is implemented by means of a video camera or camcorder or, alternatively, by means of a digital camera with video formation capabilities.
- so-called charge-coupled device (CCD) or 3CCD cameras or camcorders can be used.
- the camera or camcorder that is used for implementing the image formation device 8b is preferably a miniaturized device, i. e. a miniature camera or camcorder, so that a required installation space at respectively in the associated door structure 5 can be minimized.
- the image formation device 8b preferably comprises a backlight device 8c. This guarantees a reliable and failure-free operation of the image formation device 8b in all possible lighting conditions.
- a respective lens of the image formation device 8b is preferably coated to provide resistance to scratching, to prevent fogging and to ensure resistance to fluids commonly used in the operation and cleaning of the aircraft 1 of Figure 1 .
- the image formation device 8b preferably utilizes an already existing power supply that is e. g. running through an existing door wire harness.
- the image formation device 8b is preferentially selected from a wide range of available cameras and camcorders that are associated with a suitable backlight device and preferably comprise at least video formation capabilities and, preferentially, also still image formation capabilities.
- the real-time representation 12 can either be a video, or a still image.
- the real-time representation 12 is switchable between the video and the still image, so that the video can e. g. be used for visual inspection purposes, while the still image is used for documentation and observation purposes.
- the real-time representation 12 is suitable for determining whether the at least one lock lever 6 is in the engaged state.
- the cabin access door 4d is considered safely closed, latched and locked when the at least one lock lever 6 is engaged in the counterpart 7. Therefore, the real-time representation 12 comprises at least a representation 6a of the at least one lock lever and a representation 7a of the counterpart.
- the representation 6a of the at least one lock lever 6 corresponds to an image, i. e. a real-time visualization of the at least one lock lever 6, and the representation 7a of the counterpart 7 corresponds to an image, i. e. a real-time visualization of the counterpart 7.
- a respective current operation state of the at least one lock lever 6 and the counterpart 7 can unambiguously be determined, so that a reliable, safe and secure determination can be made on whether the at least one lock lever 6 is in the engaged state.
- the representations 6a, 7a are/is displayed on a display screen 11.
- the latter is preferably provided at a control panel 10 that, in turn, is at least provided for controlling operation of the image formation device 8b.
- the display screen 11 must not necessarily define an integral part of the control panel 10 and can likewise be provided as a separate component.
- the control panel 10 is preferably connected to the image formation device 8b by means of a suitable signal transmission connection 9.
- This signal transmission connection 9 is preferentially implemented by means of wiring or, alternatively, via a radio link, e. g. using the Bluetooth® standard.
- the control panel 10 may e. g. further be connected to another image formation device that can be used to replace e. g. a window that would otherwise be provided in the cabin access door 4d. This would enable a further reduction of cost, weight and space.
- control panel 10 and the display screen 11 can be mounted to the associated door structure 5 of the cabin access door 4d or, alternatively, to the aircraft airframe 2 of Figure 1 , preferably in the vicinity of the cabin access door 4d. Still alternatively, either one of the control panel 10 and the display screen 11 is mounted to the associated door structure 5 of the cabin access door 4d, while the other one is mounted to the aircraft airframe 2 of Figure 1 , preferably in the vicinity of the cabin access door 4d. Still alternatively, or in addition thereto, the real-time representation 12 can be transferred from the image formation device 8b to the aircraft flight deck 3c of Figure 1 for display.
- control panel 10 is configured to allow activation of the image formation device 8b and/or the display screen 11, e. g. by means of a suitable switch.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Lock And Its Accessories (AREA)
- Closed-Circuit Television Systems (AREA)
Claims (14)
- Porte de véhicule (4d) avec au moins un levier de verrouillage (6) qui est prévu pour enclencher une contrefiche (7) (1) dans une position enclenchée pour verrouiller la porte de véhicule (4d) sur le véhicule (1) associé, dans laquelle un dispositif de surveillance en temps réel (8) est prévu pour générer une représentation en temps réel (12) dudit au moins un levier de verrouillage (6) et de la contrefiche (7), la représentation en temps réel (12) étant configurée pour déterminer si ledit au moins un levier de verrouillage (6) est en position enclenchée ; caractérisée en ce que le dispositif de surveillance (8) comprend un dispositif de production d'images (8b).
- Porte de véhicule (4d) selon la revendication 1,
caractérisée en ce que le dispositif de production d'image (8b) comprend au moins des capacités de formation de vidéos animées, dans laquelle la représentation en temps réel (12) est une vidéo. - Porte de véhicule (4d) selon la revendication 2,
caractérisée en ce que le dispositif de production d'image (8b) comprend en outre des capacités de production d'images fixes, dans laquelle la représentation en temps réel (12) est permutable entre la vidéo et une image fixe. - Porte de véhicule (4d) selon la revendication 1,
caractérisée en ce qu'un élément de fixation (8a) est prévu pour fixer de façon rigide le dispositif de production d'image (8b) sur une structure de porte (5) de la porte de véhicule (4d). - Porte de véhicule (4d) selon la revendication 1,
caractérisée en ce qu'un panneau de commande (10) est prévu pour commander le fonctionnement du dispositif de production d'image (8b). - Porte de véhicule (4d) selon la revendication 5,
caractérisée en ce que le panneau de commande (10) comprend un écran d'affichage (11) pour afficher la représentation en temps réel (12). - Porte de véhicule (4d) selon la revendication 1,
caractérisée en ce que le dispositif de production d'image (8b) comprend un dispositif de rétroéclairage (8c). - Porte de véhicule (4d) selon la revendication 7,
caractérisée en ce que le véhicule (1) associé est un aéronef, dans lequel la porte de véhicule (4d) définit une porte d'accès à la cabine de l'aéronef. - Aéronef (1) avec une pluralité de portes d'aéronef (4),
caractérisé en ce que chaque porte d'aéronef (4a, 4b, 4c, 4d) est une porte de véhicule selon la revendication 1. - Aéronef (1) selon la revendication 9,
caractérisé en ce que la porte d'aéronef respective (4a, 4b, 4c, 4d) est une porte d'accès à la cabine. - Aéronef (1) selon la revendication 9,
caractérisé en ce que le dispositif de surveillance en temps réel (8) comprend un dispositif de production d'image (8b) qui comprend au moins des capacités de formation de vidéos, dans lequel la représentation en temps réel (12) est une vidéo. - Aéronef (1) selon la revendication 11,
caractérisé en ce que le dispositif de production d'image (8b) comprend en outre des capacités de production d'images fixes, dans lequel la représentation en temps réel (12) est permutable entre la vidéo et une image fixe. - Aéronef (1) selon la revendication 9,
caractérisé en ce que au moins un écran d'affichage (11) est prévu pour afficher la représentation en temps réel (12). - Aéronef (1) selon la revendication 13,
caractérisé en ce que ledit au moins un écran d'affichage (11) est prévu sur la porte d'aéronef respective (4a, 4b, 4c, 4d), à proximité de la porte d'aéronef respective (4a, 4b, 4c, 4d) et/ou sur un poste de pilotage d'aéronef (3c) de l'aéronef (1).
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP16400046.5A EP3312082B1 (fr) | 2016-10-18 | 2016-10-18 | Aéronef à portes multiples |
BR102017016713-5A BR102017016713B1 (pt) | 2016-10-18 | 2017-08-03 | Porta de veículo com pelo menos uma alavanca de trava e aeronave com uma pluralidade de portas de aeronave |
CN201710660440.3A CN107954003B (zh) | 2016-10-18 | 2017-08-04 | 具有多个飞行器门的飞行器 |
US15/784,397 US10711487B2 (en) | 2016-10-18 | 2017-10-16 | Aircraft with a plurality of aircraft doors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP16400046.5A EP3312082B1 (fr) | 2016-10-18 | 2016-10-18 | Aéronef à portes multiples |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3312082A1 EP3312082A1 (fr) | 2018-04-25 |
EP3312082B1 true EP3312082B1 (fr) | 2020-02-26 |
Family
ID=57590454
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16400046.5A Active EP3312082B1 (fr) | 2016-10-18 | 2016-10-18 | Aéronef à portes multiples |
Country Status (4)
Country | Link |
---|---|
US (1) | US10711487B2 (fr) |
EP (1) | EP3312082B1 (fr) |
CN (1) | CN107954003B (fr) |
BR (1) | BR102017016713B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11519202B2 (en) | 2020-06-09 | 2022-12-06 | The Boeing Company | Passenger door lock for drop-down style doors on an aircraft |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1992014342A1 (fr) | 1991-01-31 | 1992-08-20 | Hitwell Video, Inc. | Procede et appareil d'observation d'un trou de forage |
US5735487A (en) | 1995-12-19 | 1998-04-07 | The Boeing Company | Main deck cargo door control panel indication |
US6864805B1 (en) * | 2002-09-24 | 2005-03-08 | L-3 Communications Corporation | Surveillance system for aircraft interior |
US6659401B1 (en) * | 2002-11-13 | 2003-12-09 | Robert M. Semprini | Airplane door lock system |
US6915986B2 (en) * | 2002-11-19 | 2005-07-12 | D'alvia Graham R. | Cockpit access protection system |
US20070252038A1 (en) * | 2005-12-15 | 2007-11-01 | Domiciano Santiago Alvarez | Aerial Security and Control System |
FR2937951B1 (fr) * | 2008-10-30 | 2011-05-20 | Airbus | Systeme de surveillance et de verrouillage de portes de compartiment d'un aeronef |
DE102008059123B4 (de) | 2008-11-26 | 2013-09-19 | Airbus Operations Gmbh | Inspektionsvorrichtung für ein Fahrzeug |
CN201467356U (zh) * | 2009-03-27 | 2010-05-12 | 马扬茗 | 在飞机上应用的电子影像装置 |
US20120224058A1 (en) | 2011-03-02 | 2012-09-06 | Rosemount Aerospace Inc. | Airplane cockpit video system |
US9353550B1 (en) * | 2012-09-13 | 2016-05-31 | Shelby G. Smith, III | Lock engagement status indicator system |
CN103051874B (zh) * | 2012-12-20 | 2015-06-03 | 中国船舶重工集团公司第七二二研究所 | 一种应用于执法船上的实时高清视频监控取证系统 |
FR3004423B1 (fr) | 2013-04-12 | 2015-05-01 | Latecoere | Procede et systeme de visualisation de l'environnement externe d'un avion, ainsi que porte d'avion equipee d'un tel systeme |
US9850690B2 (en) * | 2016-02-24 | 2017-12-26 | Ford Global Technologies, Llc | Motor vehicle door lock status system and related method |
US20170362860A1 (en) * | 2016-06-16 | 2017-12-21 | Ford Global Technologies, Llc | Device for indicating lock status of a motor vehicle door |
-
2016
- 2016-10-18 EP EP16400046.5A patent/EP3312082B1/fr active Active
-
2017
- 2017-08-03 BR BR102017016713-5A patent/BR102017016713B1/pt active IP Right Grant
- 2017-08-04 CN CN201710660440.3A patent/CN107954003B/zh active Active
- 2017-10-16 US US15/784,397 patent/US10711487B2/en active Active
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
CN107954003B (zh) | 2021-07-09 |
BR102017016713B1 (pt) | 2023-04-11 |
US10711487B2 (en) | 2020-07-14 |
US20180106074A1 (en) | 2018-04-19 |
EP3312082A1 (fr) | 2018-04-25 |
CN107954003A (zh) | 2018-04-24 |
BR102017016713A2 (pt) | 2018-05-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11142321B2 (en) | Aircraft door and privacy panel assemblies | |
US9403603B2 (en) | Safety monitoring system of galley | |
US6864805B1 (en) | Surveillance system for aircraft interior | |
AU674456B2 (en) | Multi-camera closed circuit television system for aircraft | |
US4816828A (en) | Aircraft damage assessment and surveillance system | |
US10207818B2 (en) | Method and system for displaying the external environment of an aircraft, and aircraft door equipped with such a system | |
US8040257B2 (en) | Apparatus for interconnecting a pilot station to at least one other aircraft zone, cockpit and aircraft equipped with such an apparatus | |
CN109896028A (zh) | 连接飞机的集成成像系统 | |
US20140176668A1 (en) | Aircraft provided with a surveillance system | |
WO2015155379A1 (fr) | Système de surveillance de cabine et cabine d'avion ou de vaisseau spatial | |
US5735487A (en) | Main deck cargo door control panel indication | |
EP3312082B1 (fr) | Aéronef à portes multiples | |
US20190308727A1 (en) | Galley Monument For An Aircraft And Aircraft | |
US10819955B2 (en) | Aircraft provided with a surveillance system | |
BR102017007483A2 (pt) | Avian system for auxiliary in the implementation of safety measures on board of an aircraft, aircraft understanding such a system and associated method | |
CN101809635B (zh) | 用于保护航空器的起落架舱不被侵入的设备和方法 | |
US8686877B2 (en) | Directionally filtered indicator light | |
Lemmers et al. | An on-board security system and the interaction with cabin crew | |
Hůlek et al. | Pilots’ Suicides at Business and General Aviation | |
ES1069172U (es) | Circuito de seguridad para aeronaves. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
17P | Request for examination filed |
Effective date: 20180409 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20190806 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20191105 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602016030500 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1237328 Country of ref document: AT Kind code of ref document: T Effective date: 20200315 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200526 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20200226 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200626 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200526 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200527 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200719 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 1237328 Country of ref document: AT Kind code of ref document: T Effective date: 20200226 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602016030500 Country of ref document: DE |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
26N | No opposition filed |
Effective date: 20201127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201018 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20201031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201018 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200226 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20221020 Year of fee payment: 7 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230530 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231026 Year of fee payment: 8 Ref country code: DE Payment date: 20231020 Year of fee payment: 8 |